IAD05LA055
2005-04-14 · Oakland, Maryland, United States · Serious · 1 aircraft · Status: Completed
Airport 2G4
Aircraft involved
Probable cause & findings
The pilot's delay in aborting the landing, which resulted in an inadvertent stall/mush into the trees. A factor in the accident was the tailwind.
Factual narrative
On April 14, 2005, about 0720 eastern daylight time, a Cessna 337G, N53548, was destroyed when it collided with trees and caught fire following an aborted landing at the Garrett County Airport (2G4), Oakland, Maryland. The certificated private pilot and passenger were seriously injured. Visual meteorological conditions prevailed for the positioning flight that departed the Greater Cumberland Regional Airport (CBE), Cumberland, Maryland, about 0700. No flight plan was filed for the flight conducted under 14 CFR Part 91. According to the pilot, the purpose of the flight was to position the airplane at the Garrett County Airport prior to commencing aerial survey flights of the area. When the pilot departed Cumberland, the winds were "calm", and he climbed to 5,000 feet for the en route portion of the 27-mile flight. Runway 26 at Garrett County Airport was 3,001 feet long, and sat on top of a hill at 2,933 feet elevation. Trees surrounded the airport, and the terrain sloped away from the runway at the departure end of runway 26. The runway, and the treetops at the west end of the airport, were at the same approximate elevation. As the airplane approached the Garrett County Airport, the pilot announced his intention to perform a straight in approach to runway 26 over the radio, but received no response. The pilot reduced power and adjusted the flaps to approach for the descent, "but we just didn't seem to be dropping like we should." The pilot increased the flap setting and reduced the engine power further, but the approach still appeared "high." Over the runway threshold, the airplane was "a little high, and a little fast", and touched down about halfway down the runway. The pilot determined that the airplane would not stop on the remaining runway, and aborted the landing. The pilot added power, the airplane lifted from the runway, and the pilot "held the nose down" in an attempt to gain airspeed. The airplane continued off the end of the runway, and descended toward the trees. The pilot "pulled the nose up," but the airplane collided with trees and terrain. The airplane was examined at the site by a Federal Aviation Administration (FAA) aviation safety inspector on the day of the accident. The first tree strike was about 300 feet beyond the departure end of runway 26. The wreckage path was oriented 260 degrees, and continued about 150 feet to the main wreckage. The right wing was separated from the airplane, and came to rest 25 feet beyond the first tree strike. The main wreckage, which included the left wing, was consumed by fire. Several pieces of angularly cut wood were found along the wreckage path. The wood pieces were cut cleanly, at sharp angles, with the exposed wood burned by fire. One tree along the wreckage path was severed completely, and the trunk was sliced cleanly at a sharp angle. The pilot held a private pilot certificate with ratings for airplane single engine, multi-engine land, and instrument airplane. He was issued an FAA second-class medical certificate on December 15, 2004. The pilot reported approximately 1,500 hours of total flight experience, 1,100 hours of which were in multi-engine airplanes, and 900 hours of which were in make and model. At 0745, the weather reported at Garrett County Airport included clear skies with wind from 080 degrees at 8 knots. During the interview, the pilot said that during the flight, his communication radio remained tuned to the Cumberland Regional Airport UNICOM frequency of 122.8. He failed to tune the radio to the Garrett County Airport UNICOM frequency of 123.0, and was not advised of the wind and landing direction. The pilot stated that he landed with a direct tailwind of 8 knots. When asked about the handling characteristics and the performance of the airplane, he said, "It was performing perfectly," and further described the landing as a "bad decision." While on a straight-in visual approach to an non-towered airport, the pilot reduced power and adjusted the flaps to "approach" for the descent; "but we just didn't seem to be dropping like we should." The pilot increased the flap setting and reduced the engine power further, but the approach still appeared "high." Over the runway threshold, the airplane was "a little high, and a little fast", and touched down about halfway down the runway. The pilot determined that the airplane would not stop on the remaining runway, and aborted the landing. The airplane continued off the end of the runway and collided with trees and terrain. The pilot failed to tune the radio to the correct frequency, was unable to obtain the current weather conditions at the airport, and touched down with a direct tailwind of about 8 knots. When asked about the handling characteristics and the performance of the airplane, he said, "It was performing perfectly," and further described the landing as a "bad decision." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_IAD05LA055.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…